Patents by Inventor Carsten Rowedder

Carsten Rowedder has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Method for producing a rail-shaped hybrid component, and such a hybrid component
    Patent number: 10472070
    Abstract: In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component made of a titanium material is positioned on a first bar of a first profile rail that is made of a carbon-fiber reinforced plastic material and moved in an advancing direction, in a fixed position relative to the first profile rail, such that a bar portion of the first bar is arranged between a first connecting portion of the second rail component and a second connecting portion of the second rail component, and the second rail component is cohesively connected to the first profile rail. Furthermore, the hybrid component has a first profile rail made of a carbon-fiber reinforced plastic material and a second rail component made of a titanium material.
    Type: Grant
    Filed: May 18, 2017
    Date of Patent: November 12, 2019
    Assignee: AIRBUS OPERATIONS GMBH
    Inventors: Johannes Born, Alexander Gillessen, Carsten Rowedder
  • Pressure fuselage of an aircraft with a fuselage shell and a pressure bulkhead disposed therein
    Patent number: 9834298
    Abstract: A pressure bulkhead of an aircraft with a fuselage shell and a pressure bulkhead disposed therein preferably in the rear region for forming a fuselage-internal pressure region, which pressure bulkhead is attached on the edge in the interior of the fuselage shell, wherein the pressure bulkhead has a lenticular cross-section and a sandwich construction that comprises a foam core sandwiched between two opposing exterior shells.
    Type: Grant
    Filed: September 19, 2014
    Date of Patent: December 5, 2017
    Assignee: Airbus Operations GmbH
    Inventors: M. Ichwan Zuardy, Karim Grase, Carsten Rowedder, Claas De Jong, Markus Mueller, Mathias Jessrang
  • METHOD FOR PRODUCING A RAIL-SHAPED HYBRID COMPONENT, AND SUCH A HYBRID COMPONENT
    Publication number: 20170334564
    Abstract: In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component made of a titanium material is positioned on a first bar of a first profile rail that is made of a carbon-fiber reinforced plastic material and moved in an advancing direction, in a fixed position relative to the first profile rail, such that a bar portion of the first bar is arranged between a first connecting portion of the second rail component and a second connecting portion of the second rail component, and the second rail component is cohesively connected to the first profile rail. Furthermore, the hybrid component has a first profile rail made of a carbon-fiber reinforced plastic material and a second rail component made of a titanium material.
    Type: Application
    Filed: May 18, 2017
    Publication date: November 23, 2017
    Inventors: Johannes BORN, Alexander GILLESSEN, Carsten ROWEDDER
  • METHOD FOR CONNECTING METAL FITTINGS TO PIPES MADE OF FIBER-REINFORCED COMPOSITE MATERIAL, AND LINES OBTAINED WITH THIS METHOD
    Publication number: 20170015054
    Abstract: A system comprising a pipe and at least one fitting, wherein the pipe is made essentially of a thermoplastic, fiber-reinforced composite material, and the fitting is made essentially of titanium or a titanium alloy, and the pipe and the fitting are connected in a fluid-tight manner
    Type: Application
    Filed: July 14, 2016
    Publication date: January 19, 2017
    Inventors: Johannes Born, Alexander Fabritz, Carsten Rowedder
  • PRESSURE FUSELAGE OF AN AIRCRAFT WITH A FUSELAGE SHELL AND A PRESSURE BULKHEAD DISPOSED THEREIN
    Publication number: 20150008285
    Abstract: A pressure bulkhead of an aircraft with a fuselage shell and a pressure bulkhead disposed therein preferably in the rear region for forming a fuselage-internal pressure region, which pressure bulkhead is attached on the edge in the interior of the fuselage shell, wherein the pressure bulkhead has a lenticular cross-section and a sandwich construction that comprises a foam core sandwiched between two opposing exterior shells.
    Type: Application
    Filed: September 19, 2014
    Publication date: January 8, 2015
    Applicant: AIRBUS OPERATIONS GMBH
    Inventors: M. Ichwan Zuardy, Karim Grase, Carsten Rowedder, Claas DeJong, Markus Mueller, Mathias Jessrang